WO2002029917A1 - Composant de pile a combustible a oxyde solide et son procede de fabrication - Google Patents

Composant de pile a combustible a oxyde solide et son procede de fabrication Download PDF

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Publication number
WO2002029917A1
WO2002029917A1 PCT/GB2001/004410 GB0104410W WO0229917A1 WO 2002029917 A1 WO2002029917 A1 WO 2002029917A1 GB 0104410 W GB0104410 W GB 0104410W WO 0229917 A1 WO0229917 A1 WO 0229917A1
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Prior art keywords
porous gas
gas permeable
dense non
porous
solid oxide
Prior art date
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PCT/GB2001/004410
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English (en)
Inventor
Frederick James Gardner
Michael John Day
Nigel Thomas Hart
Nigel Peter Brandon
Mark Cassidy
Original Assignee
Rolls-Royce Plc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls-Royce Plc filed Critical Rolls-Royce Plc
Priority to JP2002533393A priority Critical patent/JP3934049B2/ja
Priority to AU2001292076A priority patent/AU2001292076B2/en
Priority to ES01972299T priority patent/ES2393978T3/es
Priority to DK01972299.0T priority patent/DK1332524T3/da
Priority to EP01972299A priority patent/EP1332524B1/fr
Priority to AU9207601A priority patent/AU9207601A/xx
Priority to CA2424681A priority patent/CA2424681C/fr
Publication of WO2002029917A1 publication Critical patent/WO2002029917A1/fr
Priority to US10/405,466 priority patent/US7531260B2/en
Priority to US12/405,304 priority patent/US7732075B2/en
Priority to US12/694,623 priority patent/US7892691B2/en

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/02—Details
    • H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
    • H01M8/0204—Non-porous and characterised by the material
    • H01M8/0206—Metals or alloys
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/02—Details
    • H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
    • H01M8/0204—Non-porous and characterised by the material
    • H01M8/0215—Glass; Ceramic materials
    • H01M8/0217—Complex oxides, optionally doped, of the type AMO3, A being an alkaline earth metal or rare earth metal and M being a metal, e.g. perovskites
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/02—Details
    • H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
    • H01M8/0204—Non-porous and characterised by the material
    • H01M8/0223—Composites
    • H01M8/0228—Composites in the form of layered or coated products
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/02—Details
    • H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
    • H01M8/0247—Collectors; Separators, e.g. bipolar separators; Interconnectors characterised by the form
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/02—Details
    • H01M8/0271—Sealing or supporting means around electrodes, matrices or membranes
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/10—Fuel cells with solid electrolytes
    • H01M8/12—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte
    • H01M8/1213—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte characterised by the electrode/electrolyte combination or the supporting material
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/24—Grouping of fuel cells, e.g. stacking of fuel cells
    • H01M8/241—Grouping of fuel cells, e.g. stacking of fuel cells with solid or matrix-supported electrolytes
    • H01M8/2425—High-temperature cells with solid electrolytes
    • H01M8/2428—Grouping by arranging unit cells on a surface of any form, e.g. planar or tubular
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/24—Grouping of fuel cells, e.g. stacking of fuel cells
    • H01M8/2465—Details of groupings of fuel cells
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/24—Grouping of fuel cells, e.g. stacking of fuel cells
    • H01M8/2465—Details of groupings of fuel cells
    • H01M8/2483—Details of groupings of fuel cells characterised by internal manifolds
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M4/00—Electrodes
    • H01M4/86—Inert electrodes with catalytic activity, e.g. for fuel cells
    • H01M4/90—Selection of catalytic material
    • H01M4/9016—Oxides, hydroxides or oxygenated metallic salts
    • H01M4/9025—Oxides specially used in fuel cell operating at high temperature, e.g. SOFC
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M4/00—Electrodes
    • H01M4/86—Inert electrodes with catalytic activity, e.g. for fuel cells
    • H01M4/90—Selection of catalytic material
    • H01M4/9016—Oxides, hydroxides or oxygenated metallic salts
    • H01M4/9025—Oxides specially used in fuel cell operating at high temperature, e.g. SOFC
    • H01M4/9033—Complex oxides, optionally doped, of the type M1MeO3, M1 being an alkaline earth metal or a rare earth, Me being a metal, e.g. perovskites
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M4/00—Electrodes
    • H01M4/86—Inert electrodes with catalytic activity, e.g. for fuel cells
    • H01M4/90—Selection of catalytic material
    • H01M4/9041—Metals or alloys
    • H01M4/905—Metals or alloys specially used in fuel cell operating at high temperature, e.g. SOFC
    • H01M4/9066—Metals or alloys specially used in fuel cell operating at high temperature, e.g. SOFC of metal-ceramic composites or mixtures, e.g. cermets
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M8/00—Fuel cells; Manufacture thereof
    • H01M8/10—Fuel cells with solid electrolytes
    • H01M8/12—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte
    • H01M8/1213—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte characterised by the electrode/electrolyte combination or the supporting material
    • H01M8/1226—Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte characterised by the electrode/electrolyte combination or the supporting material characterised by the supporting layer
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30—Hydrogen technology
    • Y02E60/50—Fuel cells
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50—Manufacturing or production processes characterised by the final manufactured product

Definitions

  • the present invention relates to a solid oxide fuel cell component and in particular relates to a planar solid oxide fuel cell component.
  • planar solid oxide fuel cell stack is described in European patent applications EP0668622A1 and EP0673074A1. These describe a planar solid oxide fuel cell stack comprising a plurality of solid oxide electrolyte members, each solid oxide electrolyte member having an anode electrode on a first surface and a cathode electrode on a second opposite surface to form a fuel cell. At least one interconnector is provided to connect the anode electrode of one fuel cell with the cathode electrode of an adjacent fuel cell such that the solid oxide fuel cells are connected in electrical series.
  • the fuel cells are arranged in a plane on one or both sides of a hollow porous gas permeable support/distribution member, which supplies either fuel to the anode electrodes or oxidant to the cathode electrodes.
  • the electrolytes of these solid oxide fuel cells are of the order of l ⁇ m to 50 ⁇ m, for example lO ⁇ m.
  • the main problems with all solid oxide fuel cells are the high manufacturing costs, poor thermal expansion compliance and limited operational temperature range.
  • the poor thermal expansion compliance of solid oxide fuel cells makes them intolerant to temperature differences and to thermal shocks .
  • a further problem with all solid oxide fuel cells is that the voltages are less than the Nernst value due to electrochemical and electrical losses in the fuel cells. These losses depend on the current density. The losses are due to activation in the electrodes, diffusion in the electrodes and porous gas permeable support member, electrolyte/electrode interfacial resistance, current collection in the electrodes and ionic resistance in the electrolyte. The activation losses dominate at low currents, the diffusion losses dominate at high currents and the resistive losses dominate at intermediate and high currents. Losses also arise due to current flow through the interconnectors . Also leakage losses through the electrolyte, interconnectors, and around the periphery of the fuel cells gives rise to further losses.
  • the present invention provides a solid oxide fuel cell component comprising a porous gas permeable support structure, a plurality of dense non-porous gas tight interconnectors, a dense non-porous gas tight peripheral seal layer and a plurality of solid oxide fuel cells, the solid oxide fuel cells are arranged in spaced apart relationship on a surface of the porous gas permeable support structure, the solid oxide fuel cells are arranged in electrical series, each solid oxide fuel cell comprises a dense non- porous gas tight electrolyte member, a porous gas permeable first electrode and a porous gas permeable second electrode, each dense non-porous gas tight electrolyte is arranged in contact with a corresponding one of the porous gas permeable first electrodes, each porous gas permeable second electrode is arranged in contact with a corresponding one of the dense non-porous gas tight electrolyte members, the dense non-porous gas tight interconnectors, the dense non-porous gas tight peripheral seal layer and the dense non-p
  • the dense non-porous gas tight interconnectors, the dense non-porous gas tight peripheral seal layer and the dense non-porous gas tight electrolyte members are arranged to encapsulate all of the porous gas permeable first electrodes except for the surfaces of the porous gas permeable first electrodes facing the surface of the porous gas permeable support structure to reduce leakage of reactant from the porous gas permeable first electrodes .
  • the solid oxide fuel cell stack comprises a dense non-porous gas tight seal
  • the dense non-porous gas tight electrolyte members and the dense non-porous gas tight seal are arranged to encapsulate at least one of the porous gas permeable second electrodes except for the surface of the at least one porous gas permeable second electrode remote from the dense non-porous gas tight electrolyte members to reduce leakage of reactant from the at least one porous gas permeable second electrode.
  • the dense non-porous gas tight electrolyte members and the dense non-porous seal are arranged to encapsulate all the porous gas permeable second electrodes except for the surfaces of the porous gas permeable second electrodes remote from the dense non-porous gas tight electrolyte members to reduce leakage of reactant from the porous gas permeable second electrodes.
  • Each of the porous gas permeable first electrodes is arranged in contact with the surface of the porous gas permeable support structure.
  • each of the porous gas permeable first electrodes is arranged in contact with the surface of a current collector, each current collector is arranged in contact with a porous barrier layer, the porous barrier layer is arranged in contact with the surface of the porous gas permeable support structure.
  • the at least one interconnector comprises a first layer on the porous gas permeable support structure, a second layer on the first layer and a third layer on the second layer, the first layer is dense, non-porous and is electronically and ionically non conducting, the second layer bonds the third layer to the first layer and the third layer is electronically conducting.
  • the first layer comprises a ceramic
  • the second layer comprises lanthanum chromite
  • the third layer comprises a metal
  • the third layer comprises nickel, platinum, palladium, ruthenium, silver, or an alloy two or more of the elements for example an alloy of palladium and nickel or other oxidation resistant metal.
  • the first layer comprises yttria stabilised zirconia doped with silicate glass or yttria stabilised zirconia doped with calcium chromate such that the barrier layer is ionically non conducting.
  • the at least one interconnector comprises a first layer on the porous gas permeable support structure and a second layer on the first layer, the first layer is dense, non-porous and is electronically and ionically non conducting and the second layer is electronically conducting.
  • the first layer comprises a ceramic and the second layer comprises a metal.
  • the second layer comprises nickel, platinum, palladium, ruthenium, silver, or an alloy of two or more of the elements for example an alloy of palladium and nickel.
  • the first layer comprises yttria-stabilised zirconia.
  • the first layer comprises yttria stabilised zirconia doped with silicate glass or yttria stabilised zirconia doped with calcium chromate such that the first layer is ionically non conducting.
  • the dense non-porous gas tight peripheral seal extends around the periphery of the area defined by the porous gas permeable first electrodes and the dense non-porous interconnectors.
  • the ends of the dense non-porous interconnectors overlap the dense non-porous gas tight peripheral seal .
  • the edges of the dense non- porous gas tight electrolyte members overlap the dense non- porous gas tight peripheral seal.
  • the dense non-porous gas tight peripheral seal comprises a first layer and a second layer.
  • the dense non-porous gas tight peripheral seal comprises a ceramic.
  • the dense non-porous gas tight peripheral seal comprises yttria-stabilised zirconia.
  • the dense non-porous gas tight peripheral seal comprises yttria stabilised zirconia doped with silicate glass or yttria stabilised zirconia doped with calcium chromate such that the dense non-porous gas tight seal is ionically non conducting.
  • the dense non-porous seal overlaps the dense non-porous gas tight peripheral seal.
  • the dense non-porous seal overlaps the ends of the dense non- porous gas tight electrolytes.
  • the dense non- porous seal overlaps the ends of the dense non-porous interconnectors.
  • the dense non-porous seal comprises a glass ceramic material .
  • the porous gas permeable substrate comprises a ceramic with a thermal expansion coefficient macched to that of the dense non-porous gas tight electrolyte member.
  • the ceramic comprises a mixture of magnesium aluminate and magnesia.
  • the ceramic comprises calcia-stabilised zirconia.
  • each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte member may be in sealing contact with the surface of the porous gas permeable support structure.
  • each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte member overlaps one of the interconnectors.
  • each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte member abuts one of the interconnectors.
  • each porous gas permeable first electrode overlaps one of the interconnectors.
  • each porous gas permeable first electrode overlaps one of the interconnectors.
  • the present invention also provides a method of manufacturing a solid oxide fuel cell component comprising a porous gas permeable support structure, a plurality of dense interconnectors, a dense non-porous gas tight peripheral seal layer and a plurality of solid oxide fuel cells, the solid oxide fuel cells are arranged in spaced apart relationship on a surface of the porous gas permeable support structure, the solid oxide fuel cells are arranged in electrical series, each solid oxide fuel cell comprises a dense non- porous gas tight electrolyte member, a porous gas permeable first electrode and a porous gas permeable second electrode, each dense non-porous gas tight electrolyte is arranged in contact with a corresponding one of the porous gas permeable first electrodes, each porous gas permeable second electrode is arranged in contact with a corresponding one of the dense non-porous gas tight electrolyte members, each of the porous gas permeable first electrode
  • step (e) depositing a plurality of porous gas permeable second electrodes on the plurality of dense non-porous gas eight electrolyte members.
  • step (d) comprises depositing the plurality of dense non-porous gas tight electrolyte members on the porous gas permeable first electrodes such that the dense non-porous interconnectors, the dense non-porous gas tight peripheral seal layer and the dense non-porous gas tight electrolyte members are arranged to encapsulate all of the porous gas permeable first electrodes except for the surfaces of the porous gas permeable first electrodes in contact with the surface of the porous gas permeable support structure to reduce leakage of reactant from the porous gas permeable first electrodes.
  • the method comprises the subsequent step of:-
  • step (f) comprises depositing the dense non-porous seal around the plurality of porous gas permeable second electrodes such that the dense non-porous gas tight electrolyte members and the dense non-porous seal encapsulate all the porous gas permeable second electrodes except for the surfaces of the porous gas permeable second electrodes remote from the dense non-porous gas tight electrolyte members to reduce leakage of reactant from the porous gas permeable second electrodes.
  • step (a) comprises depositing the dense non-porous gas tight peripheral seal such that it extends around the periphery of the area defined by the porous gas permeable first electrodes and the dense non-porous interconnectors .
  • step (a) comprises depositing the dense non-porous interconnectors such that they overlap the dense non-porous gas tight peripheral seal.
  • step (d) comprises depositing the dense non-porous gas tight electrolyte members such that they overlap the dense non-porous gas tight peripheral seal.
  • step (a) comprises depositing a first layer and a second layer to form the dense non-porous gas tight peripheral seal.
  • the dense non-porous gas tight peripheral seal comprises a ceramic.
  • the dense non-porous gas tight peripheral seal comprises yttria- stabilised zirconia.
  • step (f) comprises depositing the dense non-porous seal such that it overlaps the dense non-porous gas tight peripheral seal.
  • step (f) comprises depositing the dense non-porous seal such that it overlaps the ends of the dense non-porous gas tight electrolyte members.
  • step (f) comprises depositing the dense non-porous seal such that it overlaps the ends of the dense non-porous interconnectors.
  • step (d) comprises depositing the dense non-porous gas tight electrolyte members such that one end of each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte member is in sealing contact with the surface of the porous gas permeable support structure.
  • Step (d) may comprise depositing the dense non-porous gas tight electrolyte members such that one end of each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte members abut one of the interconnectors .
  • step (d) may comprise depositing the dense non-porous gas tight electrolyte members such that one end of each dense non-porous gas tight electrolyte member overlaps one of the interconnectors and the second end of each dense non-porous gas tight electrolyte member overlaps one of the interconnectors.
  • step (c) comprises depositing the porous gas permeable first electrodes such that one edge of each porous gas permeable first electrode overlaps one of the interconnectors .
  • step (c) comprises depositing the porous gas permeable first electrodes such that the whole of each porous gas permeable first electrode overlaps one of the interconnectors .
  • the method comprises the additional steps of:- (g) sintering after step (d) and before step (e) and
  • step (h) sintering after step (f) .
  • the method comprises the additional steps of:-
  • step (i) sintering after step (f) .
  • the method comprises the additional steps of : -
  • step (i) sintering after step (c) and before step (d) ,
  • step (j) sintering after step (d) and before step (e)
  • step (k) sintering after step (e) and before step (f)
  • step (f) sintering after step (f) .
  • Figure 1 is a partially cut away perspective view of a solid oxide fuel cell stack according to the present invention.
  • Figure 2 is a plan view of one component of the solid oxide fuel cell stack shown in figure 1.
  • Figure 3 is an enlarged cross-sectional view along line A-A through the component of the solid oxide fuel cell stack shown in figure 2.
  • Figure 4 is a cross-sectional view along line B-B through the component of the solid oxide fuel cell stack shown in figure 3.
  • Figure 5 is a cross-sectional view along line C-C through the solid oxide fuel cell component shown in figure 3.
  • Figures 6A to 6E illustrate the manufacturing sequence for making the solid oxide fuel cell stack component shown in figures 3 to 5.
  • Figure 7 is a further enlarged cross-sectional view through the solid oxide fuel cell component shown in figure 3.
  • Figure 8 is an alternative enlarged cross-sectional view along line A-A through the solid oxide fuel cell component shown in figure 2.
  • Figure 9 is a further enlarged cross-sectional view through the solid oxide fuel cell component shown in figure 8.
  • Figure 10 is a further enlarged cross-sectional view along line A-A through the solid oxide fuel cell component shown in figure 2.
  • Figure 11 is a further enlarged cross-sectional view through the solid oxide fuel cell component shown in figure 10.
  • a solid oxide fuel cell stack 10 according to the present invention is shown in figures 1 to 5 and 7.
  • the solid oxide fuel cell stack 10 comprises at least one, preferably a plurality of components 12 arranged within a casing 14.
  • Each component 12, as shown more clearly in figures 2 to 5 comprises a hollow porous gas permeable support structure 16 which has an internal surface 18 and an external surface 22.
  • the internal surface 18 of the hollow porous gas permeable support structure 16 at least partially defines one or more chambers 20 for the supply of a first reactant to the internal surface 18 of the porous gas permeable support structure 16.
  • the external surface 22 of the hollow porous gas permeable support structure 16 supports a plurality of solid oxide fuel cells 24 which are arranged in spaced apart relationship on the external surface 22 of the hollow porous gas permeable support structure 16.
  • a second reactant is supplied to the external surface 22 of the hollow porous gas permeable support structure 16.
  • the solid oxide fuel cells 24 are electrically interconnected in series.
  • Each solid oxide fuel cell 24, as shown more clearly in figures 3, 4, 5 and 7 comprises a porous gas permeable first electrode 26, a dense non-porous gas tight electrolyte member 28 and a porous gas permeable second electrode 30.
  • a plurality of dense non-porous gas tight interconnectors 32 are provided. At least one, all except two of the, dense non-porous gas tight interconnector 32 is arranged to interconnect the first electrode 26 of one solid oxide fuel cell 24 with the second electrode 30 of an adjacent solid oxide fuel cell 24.
  • Each dense non-porous gas tight interconnector 32 is arranged on the external surface 22 of the porous gas permeable support structure 16, most of the dense non-porous gas tight interconnectors 32 are positioned in the space between two adjacent solid oxide fuel cells 24.
  • a dense non-porous gas tight interconnector 32A is arranged at a first end of the solid oxide fuel cell stack to interconnect the porous gas permeable first electrode 26 of one solid oxide fuel cell 24 with a first terminal 36.
  • a dense non-porous gas tight interconnector 32B is arranged at a second end of the solid oxide fuel cell stack to interconnect the porous gas permeable second electrode 30 of one solid oxide fuel cell 24 with a second terminal 37.
  • porous gas permeable first electrode 26 of each solid oxide fuel cell 24 is arranged on the external surface 22 of the porous gas permeable support structure 16, as shown in figures 3, 4, 5 and 7.
  • a dense non-porous gas tight peripheral seal layer 34 is arranged on the external surface 22 of the porous gas permeable support structure 16 on the periphery of the area defined by the porous gas permeable first electrodes 26 and the dense non-porous gas tight interconnectors 32, 32A and 32B.
  • a first end 26A of each porous gas permeable first electrode 26 is arranged to contact one of the dense non- porous gas tight interconnectors 32.
  • a second end 26B of each porous gas permeable first electrode 26 is arranged in spaced part relationship with an adjacent one of the dense non-porous gas tight interconnectors 32.
  • Each dense non-porous gas tight electrolyte 28 is arranged in contact with a corresponding one of the porous gas permeable first electrodes 26.
  • a first end 28A of each dense non-porous gas tight electrolyte 28 is arranged in sealing contact with one of the dense non-porous gas tight interconnectors 32.
  • a second end 28B of each dense non- porous gas tight electrolyte 28 is arranged between the second end 26B of the porous gas permeable first electrode 26 and the adjacent one of the dense non-porous gas tight interconnectors 32.
  • the second end 28B of the dense non- porous gas tight electrolyte member 28 is in sealing contact with the external surface 22 of the porous gas permeable support structure 16.
  • each dense non-porous gas tight electrolyte 28 is also in sealing contact with the adjacent one of the dense non- porous gas tight interconnectors 32.
  • the edges 28C and 28D of each dense non-porous gas tight electrolyte 28 are in sealing contact with the dense non-porous gas tight peripheral seal layer 34 to encapsulate the porous gas permeable first electrodes 26 to prevent gas leakage from the porous gas permeable first electrodes 26.
  • Each porous gas permeable second electrode 30 is arranged in contact with a corresponding one of the dense non-porous gas tight electrolytes 28.
  • a first end 30A of each porous gas permeable second electrode 30 is spaced from a second end 30B of an adjacent porous gas permeable second electrode 30.
  • the second end 30B of each porous gas permeable second electrode 30 is arranged in contact with the adjacent one of the dense non-porous gas tight interconnectors 32. It is to be noted that the second end 30B of the porous gas permeable second electrode 30 of each solid oxide fuel cell 24 is spaced from the dense non-porous gas tight electrolyte 28 of an adjacent solid oxide fuel cell 24 to prevent the formation of spurious solid oxide fuel cells .
  • a dense non-porous gas tight seal 38 is arranged between the porous gas permeable second electrodes 30 and is in sealing contact with a portion of the dense non- porous gas tight electrolytes 28 and the dense non-porous gas tight interconnectors 32.
  • the dense non-porous gas tight seal 38 is also arranged around the periphery of the area defined by the porous gas permeable second electrodes 30 and is in sealing contact with the dense non-porous gas tight peripheral seal layer 34.
  • the dense non-porous gas tight seal 38 penetrates into the edges of the porous gas permeable second electrodes 30 which contact the edges of the dense non-porous gas tight electrolyte 28 and the edges of the surface of the dense non-porous gas tight interconnector 32.
  • the infiltration of the dense non-porous gas tight seal 38 into the edges of the porous gas permeable second electrodes 30 forms a further seal in the event of a leakage of gas from the porous gas permeable first electrodes 26 through the dense non-porous gas tight interconnectors 32.
  • the porous gas permeable support structure 16 preferably comprises magnesia doped magnesium aluminate, however calcia stabilised zirconia or other suitable ceramics may be used.
  • the magnesium aluminate is preferred because it is cheaper and has lower density than calcia stabilised yttria, and additionally the magnesium aluminate has negligible ion conductivity.
  • the magnesium aluminate is doped with magnesia to match the thermal expansion coefficient of the yttria stabilised zirconia electrolyte, thus the magnesia doped magnesium aluminate is produced by mixing 60-70wt% magnesia and balance alumina.
  • the calcia- stabilised zirconia must have a dopant level of greater than 16mol% calcia to ensure the zirconia is fully stabilised, for example 7wt% calcia.
  • One advantage of calcia stabilised zirconia is that it has a thermal expansion coefficient matched to the dense non-porous gas tight electrolytes. The calcia stabilised zirconia does not react with the other components of the fuel cells during sintering and the calcia stabilised zirconia has a lower oxygen ion conductivity than yttria stabilised zirconia.
  • the first layer 40 on the porous gas permeable support structure, is a dense non- porous gas tight barrier layer which is neither ionically conducting or electronically conducting and for example comprises yttria stabilised zirconia containing a dopant, for example l-2wt% silicate glass material or 0.02-4wt% calcium chromate.
  • the dopants reduce the oxygen ion conductivity and act as sintering aids.
  • the second layer 42 is a bond coating for the third layer and for example comprises lanthanum chromite. The second layer improves the densification of the first layer and reduces the ionic conductivity of the first layer.
  • the second layer is about lO ⁇ m thick after sintering.
  • the third layer 44 is electronically conducting and oxidation resistant and comprises nickel, platinum, palladium, ruthenium, silver or an alloy of any two or more of nickel, platinum, palladium, ruthenium and silver, for example an alloy of palladium and nickel or other suitable metal.
  • the platinum is sintered into the lanthanum chromite such that about 50% of the surface area of the interconnector is platinum and about 50% is lanthanum chromite.
  • each interconnector 32, 32A, 32B comprises a first layer, on the porous gas permeable support structure, and a second layer on the first layer.
  • the first layer is dense non-porous gas tight and is electronically and ionically non-conducting and the second layer is electronically conducting.
  • the first layer comprises a ceramic and the second layer comprises a metal.
  • the metal comprises nickel, platinum, palladium, ruthenium, silver or an alloy of any two or more of nickel, platinum, palladium, ruthenium and silver, for example an alloy of 80wt% palladium and 20wt% nickel or other oxidation resistant metal.
  • the first layer 40 of the interconnectors 32, 32A and 32B may be deposited in two layers such that the yttria scabilised zirconia and dopants firstly fills the pores in the hollow porous gas permeable support structure 16 and then produces a smooth pore free surface.
  • the dense non-porous gas tight peripheral seal layer 34 is a dense non-porous gas tight barrier layer which is neither ionically conducting or electronically conducting and for example comprises yttria stabilised zirconia containing a dopant, for example l-2wt% silicate glass material or 0.02-4wt% calcium chromate.
  • the dopants reduce oxygen ionic conductivity and act as sintering aids.
  • the dense non-porous gas tight barrier peripheral seal 34 may be deposited in two layers such that the yttria stabilised zirconia firstly fills the pores in the hollow porous gas permeable support structure 16 and then produces a smooth pore free surface.
  • the first electrode, anode, 26 comprises 60wt% nickel oxide and 40 wt% yttria stabilised zirconia.
  • the yttria- stabilised zirconia comprises 8wt% yttria.
  • the sintered anode thickness is about 30 ⁇ m.
  • the hollow porous gas permeable support structure 16 comprises magnesia doped magnesium aluminate a barrier layer is deposited on to the hollow porous gas permeable support structure 16 before the first electrode 26, because the nickel oxide reacts with the alumina in the magnesium aluminate.
  • the barrier layer must layer prevent this reaction occurring and must be porous to allow reactants to flow to and from the anode 26.
  • the barrier layer comprises 8wt% yttria stabilised zirconia.
  • the porous gas permeable first electrode, anode, 26 comprises nickel, palladium and ceria.
  • the porous gas permeable first electrode 26 may comprise ceria, a ceria/nickel or palladium cermet, or ceria with an electronic conducting current distribution mesh of nickel or palladium or nickel/palladium alloy.
  • the dense non-porous gas tight electrolytes 28 comprise 8wt% yttria stabilised zirconia and an oxide to aid sintering.
  • the oxide may be lwt% alumina, lmol% alumina and lmol% titania, 5mol% titania, lwt% nickel oxide or 0.25wt% boron oxide.
  • the dense non-porous gas tight electrolytes 28 have a density of greater than 98%.
  • the electrolytes 28 may comprise yttria stabilised zirconia with two different particle sizes, for example an average particle size of about 0.7 micrometers and an average particle size of about 0.1 micrometers to enable good sintering to obtain maximum density without shrinkage and delamination of the electrolytes 28.
  • the thickness of the dense non-porous gas tight electrolytes 28 is about lO ⁇ m.
  • the porous gas permeable second electrode, cathode electrode, 30 comprises a first layer and a second layer.
  • the first layer comprises 50wt% 8wt% yttria stabilised zirconia and 50wt% lanthanum strontium manganite (La 0 8 Sr 0-15 Mn0 3 ) .
  • the mixture of yttria stabilised zirconia and lanthanum strontium manganite provides enhanced oxygen ion conductivity for the first layer, increasing the effective area of the porous gas permeable second electrode 30/dense non-porous gas tight electrolyte 28 interface.
  • the first layer is between 5 and 15 ⁇ m thick.
  • the second layer comprises 100wt% lanthanum strontium manganite having a larger particle size than the first layer.
  • the second layer improves the electronic conductance of the second electrode 30.
  • the larger particle size improves the lateral conductivity and sintering characteristics to produce a porous crack free second electrode 30.
  • the second layer is between 50 and 150 ⁇ m thick.
  • the porous gas permeable second, cathode, electrode 30 may comprise lanthanum strontium manganite/ceria composite.
  • the dense non-porous gas tight seal 38 comprises a glass ceramic for example a barium oxide silica alumina based glass material which contains zircon which forms a glass ceramic film. Other suitable glass ceramics may be used.
  • the terminals 36 and 37 comprise nickel aluminide, and are formed by placing an aluminium layer on the substrate 16 and placing a nickel lug in contact with the aluminium layer. The aluminium and nickel react at the sintering temperature to form nickel aluminide to bond the terminal 36, 37 to the lug and the interconnector 32A, 32B.
  • the terminals 36 and 37 comprise 80wt% palladium and 20wt% nickel.
  • the solid oxide fuel cell component is manufactured by forming the porous gas permeable support structure 16 by producing a ceramic dough of the calcia stabilised zirconia, or magnesia doped magnesium aluminate, by mixing powdered ceramic with an aqueous organic matrix.
  • the ceramic dough is then passed through a ram extruder using a die to produce the porous gas permeable support structure shown in figures 3, 4 and 5 although other shapes may be produced.
  • the porous gas permeable support structure 16 is dried for a suitable period of time. Microwave or others suitable drying may be used to accelerate the drying process.
  • the dried porous gas permeable support structure 16 is machined by cutting, grinding, milling, linishing and drilling using conventional tools. The machining is used to form manifolds, or interconnections, at the ends of the porous gas permeable support structure 16.
  • the ends of the porous gas permeable support structure 16 may be sealed with a cap of the dried extruded ceramic dough and or a paste of the ceramic dough and dried.
  • the porous gas permeable support structure 16 is then sintered in a furnace on zirconia balls, which allow movement of the porous gas permeable support structure 16.
  • the porous gas permeable support structure is sintered at a temperature of 1400°C for a suitable time, for example two hours, to allow the temperature of the porous gas permeable support structure 16 to become equal at all points. This enables uniform sintering of the porous gas permeable support structure 16.
  • a plurality of first layers 40 of dense non-porous barrier layer of the dense non-porous gas tight interconnectors 32 and the dense non-porous gas tight peripheral seal layer 34 are deposited on the porous gas permeable support structure 16, as shown in figure 6A.
  • a base coat of calcia stabilised zirconia, or other suitable ceramic is applied by dip coating to fill in the porosity of the porous gas permeable support structure 16, the calcia stabilised zirconia has a particle size less than 2 ⁇ m and is applied as a water based slurry.
  • the base coat is then fired at 1400°C for 1 hour.
  • the topcoat is applied by screen-printing using a common screen, the topcoat is yttria-stabilised zirconia comprising a dopant as discussed previously.
  • a plurality of second layers 42 and third layers 44 of the dense non-porous gas tight interconnectors 32 are deposited on the first layers 40 of the dense non-porous gas tight interconnectors 32 as shown in figure 6B.
  • the second layers 42 and third layers 44 overlap the dense non- porous gas tight peripheral seal layer 34.
  • the second and third layers 42 and 44 of the dense non-porous gas tight interconnectors 32 are deposited by screen-printing.
  • a plurality of porous gas permeable first electrodes 26 are deposited on the porous gas permeable support structure 16.
  • the porous gas permeable first electrodes 26 overlap one of the adjacent dense non-porous gas tight interconnectors 32 but are spaced from the other of the adjacent dense non-porous gas tight interconnectors 32, as shown in figure 6C.
  • the porous gas permeable first electrodes 26 are deposited by screen-printing.
  • a plurality of dense non-porous gas tight electrolytes 28 are deposited on the porous gas permeable first electrodes 26 such that the dense non-porous gas tight interconnectors 32, the dense non-porous gas tight peripheral seal layer 34 and the dense non-porous gas tight electrolytes 28 are arranged to encapsulate all of the porous gas permeable first electrodes 26, as shown in figure 6D, except for the surface of the porous gas permeable first electrodes 26 in contact with the surface of the porous gas permeable support structure 16 to reduce, preferably prevent, leakage of reactant from the porous gas permeable first electrodes 26.
  • the dense non-porous gas tight electrolytes 28 overlap the dense non-porous gas tight peripheral seal layer 34.
  • Each dense non-porous gas tight electrolyte 28 overlaps one dense non-porous gas tight interconnector 32 and abuts the other dense non- porous gas tight interconnector 32.
  • the dense non-porous gas tight electrolytes 28 are deposited by screen-printing.
  • the electrolytes 28 may be deposited by depositing a layer comprising yttria stabilised zirconia particles with the average particle size of about 0.7 micrometers which produces 98% density.
  • a second layer may be deposited by depositing a mixture of yttria stabilised zirconia particles with an average particle size of 0.7 micrometers and yttria stabilised zirconia particles with an average particle size of 0.1 micrometers.
  • a plurality of porous gas permeable second electrodes 30 are deposited on the plurality of dense non-porous gas tight electrolytes 28, as shown in figure 6E.
  • the porous gas permeable second electrodes 30 overlap the dense non- porous gas tight interconnectors 32.
  • the porous gas permeable second electrode 30 of each solid oxide fuel cell is spaced from the dense non-porous gas tight electrolyte 28 of an adjacent solid oxide fuel cell to prevent the formation of spurious solid oxide fuel cells.
  • the porous gas permeable second electrodes 30 are deposited by stencil printing, or slurry spraying, to minimise damage to the underlying dense non-porous gas tight electrolytes 28.
  • the dense non-porous gas tight seal 38 is deposited around the plurality of porous gas permeable second electrodes 30 such that the dense non-porous gas tight electrolytes 28 and the dense non-porous gas tight seal layer 38 encapsulates all the porous gas permeable second electrodes 30 except for the surfaces of the porous gas permeable second electrodes 30 remote from the dense non- porous gas tight electrolytes 28.
  • the dense non-porous gas tight seal 38 is deposited by screen-printing.
  • a sintering step after the dense non-porous gas tight peripheral seal layer 34 and dense non-porous gas tight interconnectors 32 have been deposited.
  • a further sintering step after the porous gas permeable first electrodes 26 and dense non- porous gas tight electrolytes 28 have been deposited and a further sintering step after the porous gas permeable second electrodes 30 and dense non-porous gas tight seal 38 has been deposited.
  • sintering steps comprise heating to temperatures between 1000°C and 1500°C.
  • the interconnectors 32 are sintered at a temperature in the range 1300°C to 1500°C
  • the anode electrodes 26 and electrolytes 28 are sintered at a temperature in the range the 1400°C to 1450°C
  • the cathode electrodes 30 are sintered at a temperature in the range 1000°C to 1400°C.
  • the arrangement allows the dense non-porous gas tight interconnectors 32 and dense non-porous gas tight peripheral seal layer 34 to be sintered at high temperatures to make them dense, non-porous and gas tight without unwanted chemical reactions with other layers.
  • the sintering temperature is reduced as each layer is deposited.
  • the porous gas permeable support structure 16 has two parallel planar surfaces and that one or both of the planar surfaces may be provided with solid oxide fuel cells.
  • a cross-section through an alternative solid oxide fuel cell component 112, is shown more clearly in figures 8 and 9.
  • the component 112 comprises a hollow porous gas permeable support structure 116, which has an internal surface 118 and an external surface 122.
  • the internal surface 118 of the hollow porous gas permeable support structure 116 at least partially defines one or more chambers 120 for the supply of a first reactant to the internal surface 118 of the porous gas permeable support structure 116.
  • the external surface 122 of the hollow porous gas permeable support structure 116 supports a plurality of solid oxide fuel cells 124 which are arranged in spaced apart relationship on the external surface 122 of the hollow porous gas permeable support structure 116.
  • a second reactant is supplied to the external surface 122 of the hollow porous gas permeable support structure 16.
  • the solid oxide fuel cells 124 are electrically interconnected in series.
  • Each solid oxide fuel cell 124 comprises a porous gas permeable first electrode 126, a dense non-porous gas tight electrolyte member 128 and a porous gas permeable second electrode 130.
  • a plurality of dense non-porous gas tight interconnectors 132 are provided. At least one, all except two of the, dense non-porous gas tight interconnector 132 is arranged to interconnect the porous gas permeable first electrode 126 of one solid oxide fuel cell 124 with the porous gas permeable second electrode 130 of an adjacent solid oxide fuel cell 124.
  • each solid oxide fuel cell 124 is arranged on a respective one of a plurality of porous gas permeable current collectors 135.
  • Each porous gas permeable current collector 135 is arranged on a respective one of a plurality of porous gas permeable barrier layers 123.
  • Each dense non-porous gas tight interconnector 132 comprises a dense non-porous gas tight barrier layer 134 on the surface 122 of the porous gas permeable support structure 116 and an electronically conducting and oxidation resistant layer 133 on the dense non-porous gas tight barrier layer 134.
  • the dense non- porous gas tight barrier layer 134 and the porous gas permeable barrier layer 123 prevent chemical interactions between the porous gas permeable first electrode 126 and the porous gas permeable support structure 116.
  • Most of the dense non-porous gas tight interconnectors 132 are positioned in the space between two adjacent solid oxide fuel cells 124.
  • a dense non-porous gas tight interconnector 132A is arranged at one end of the solid oxide fuel cell component to interconnect the porous gas permeable first electrode 126 of one solid oxide fuel cell 124 with a first terminal 36.
  • a dense non-porous gas tight interconnector 132B is arranged at one end of the solid oxide fuel cell component to interconnect the porous gas permeable second electrode 130 of one solid oxide fuel cell 124 with a second terminal 37.
  • the dense non-porous gas tight peripheral seal layer 134 is arranged on the external surface 122 of the porous gas permeable support structure 116 on the periphery of the area defined by the porous barrier layer 123.
  • each porous gas permeable first electrode 126 is arranged to contact the respective current collector 135.
  • Each dense non-porous gas tight electrolyte 128 is arranged in contact with a corresponding one of the porous gas permeable first electrodes 126.
  • a first end 128A of each dense non-porous gas tight electrolyte 128 is arranged in sealing contact with the dense non-porous barrier layer 134 of a dense non-porous gas tight interconnector 132.
  • a second end 128B of each dense non-porous gas tight electrolyte 128 is arranged in sealing contact with layer
  • each dense non-porous gas tight electrolyte 128 is in sealing contact with the dense non-porous gas tight peripheral seal layer
  • Each porous gas permeable second electrode 130 is arranged in contact with a corresponding one of the dense non-porous gas tight electrolytes 128.
  • a first end 130A of each porous gas permeable second electrode 130 is spaced from a second end 13OB of an adjacent porous gas permeable second electrode 130.
  • the second end 130B of each porous gas permeable second electrode 130 is arranged in contact with the adjacent one of the interconnectors 132.
  • the second end 130B of each porous gas permeable second electrode 130 is spaced from the dense non-porous gas tight electrolyte 128 of an adjacent fuel cell 124 to prevent the formation of spurious solid oxide fuel cells.
  • a dense non-porous gas tight seal 138 is arranged between the porous gas permeable second electrodes 130 and is in sealing contact with a portion of the dense non- porous gas tight electrolytes 128.
  • the dense non-porous gas tight seal 138 is also arranged around the periphery of the area defined by the porous gas permeable second electrodes 130 and is in sealing contact with the dense non-porous gas tight peripheral seal layer 134.
  • the dense non-porous gas tight peripheral seal layer 134 is also in sealing contact with the interconnectors 132.
  • the dense non-porous gas tight seal 138 penetrates into the edges of the porous gas permeable second electrodes 130, which contact the edges of the dense non- porous gas tight electrolyte member 128, and the surface of layer 133 of the dense non-porous gas tight interconnectors 132 that is not contacted by the dense non-porous gas tight electrolyte member 128 and not contacted by the porous gas permeable second electrodes 130.
  • the infiltration of the dense non-porous gas tight seal 138 into the edges of the porous gas permeable second electrodes 130 forms a further seal in the event of a leakage of gas from the porous gas permeable first electrodes 126 through the dense non-porous gas tight interconnectors 132.
  • This arrangement is produced by firstly depositing the porous gas tight barrier layer 123 and the dense non-porous gas tight peripheral barrier layer 134. Then secondly the layer 133 of the interconnectors 132 and current collectors 135 are deposited and the assembly is sintered at high temperatures so as to prevent subsequent chemical reactions. Then the porous gas permeable first electrodes 126 are deposited, followed by the dense non-porous gas tight electrolyte members 128, followed by the porous gas permeable second electrodes 130 and finally the dense non- porous gas tight seal 138.
  • the current collectors 135 and layers 133 of the interconnectors 132 are integral and are arranged between the porous gas permeable first electrodes 126 and the porous gas permeable support structure 116.
  • the current collectors 135 are porous and gas permeable to allow the first reactant to flow from the porous gas permeable support structure 116 to the porous gas permeable first electrodes 126.
  • the current collectors 135 collect current from/supply current to the first porous gas permeable first electrodes 126.
  • the current collectors 135 and layers 133 of the interconnectors 132 have high lateral, in plane, conductivity.
  • the current collectors 135 and layers 133 of the interconnectors 132 are relatively thin, of the order of a few micrometers thick.
  • the length of the current collector 135 and layer 133 of the interconnector 132 is relatively long, of the order of several mm long.
  • any leakage path is long and narrow and leakage is minimal or substantially zero.
  • each fuel cell is about 15mm long and about 0.030mm thick, the current collector 135 and layer 133 of the interconnector 132 is almost 15mm long and about 1 micrometer thick.
  • the layer 133 of the interconnector 132 is substantially gas tight for flow in a lateral direction.
  • the current collectors 135 and layers 133 of the interconnectors 132 comprise at least one of nickel, platinum, palladium, ruthenium and silver, preferably two or more of these, for example nickel and platinum or nickel and palladium, nickel and ruthenium etc.
  • the interconnectors 132 also comprise yttria-stabilised zirconia to aid bonding of the interconnector 132 to the porous- barrier layer 123 and dense non-porous gas tight barrier layer 134.
  • a porous gas permeable current collector 131 is arranged on the porous gas permeable second electrode 130 to collect current from/supply current to the second porous gas permeable second electrodes 130.
  • the current collectors 131 have high lateral, in plane, conductivity.
  • the current collectors 131 comprise a high conductivity metal or alloy for example one or more of nickel and silver and one or more of platinum, palladium ruthenium and gold, for example nickel and platinum, nickel and palladium, nickel and ruthenium etc.
  • the current collector 131 is deposited by screen printing and doctor blading and is about 10 micrometers thick.
  • first electrodes 26 are anode electrodes and the second electrodes 30 are cathode electrodes.
  • a cross-section through an alternative solid oxide fuel cell component 212 is shown more clearly in figures 10 and 11.
  • the component 212 is substantially the same as that shown in figures 3, 4, 5 and 7 and like parts are denoted by like numerals.
  • the component 212 in figures 10 and 11 differs in that the second end 28B of each dense non-porous gas tight electrolyte member 28 abuts and overlaps the adjacent dense non-porous gas tight interconnector 32.
  • porous barrier layers 123 are arranged between each porous gas permeable first, anode, electrode 26 and the porous gas permeable support structure 16 to prevent chemical interactions between the porous gas permeable anode electrodes 26 and the porous gas permeable support structure 16.
  • porous gas permeable barrier layer it may be possible to deposit a porous gas permeable barrier layer over the whole surface of the porous gas permeable support structure to prevent chemical interactions between the porous gas permeable support structure and the porous gas permeable first electrodes.
  • a dense non-porous gas tight barrier layers is subsequently provided at appropriate positions over the porous gas permeable barrier layer for the interconnectors.
  • the dense non-porous gas tight peripheral seal is provided over the remaining surface of the porous gas permeable support structure .
  • the first electrodes as anode electrodes it may be possible that the first electrodes are cathode electrodes.
  • the reactant supplied to the anode is generally hydrogen or the products of reformation of a hydrocarbon fuel, for example hydrogen, carbon dioxide, carbon monoxide.
  • the reactant supplied to the cathode is generally oxygen, air or other oxygen containing gas.
  • the arrangement of the fuel cells enables the dense non-porous gas tight layers to be deposited initially and fired at the highest temperatures to obtain the sintering to form the dense non-porous gas tight layers.
  • the other layers are deposited and fired at progressively lower temperatures. This enables the solid oxide fuel cells to operate at temperatures up to 1200°C.
  • the length and thickness of the layers of the solid oxide fuel cell stack are important design variables and influence the solid oxide fuel cell stack performance. Current collection losses are minimised by minimising the length of any current path. This is achieved by minimising the pitch of the solid oxide fuel cells.
  • the pitch of the solid oxide fuel cells is length of the electrolyte member plus the length of the interconnector. Resistance to flow of current is minimised by minimising the number of interfaces. These conflicting requirements result in an optimum solid oxide fuel cell pitch, the magnitude of which depends upon the thickness and conductivity of the anode and cathode current collectors.
  • the pitch of solid oxide fuel cell is between 5mm and 20mm.
  • the electrolyte member/interconnector aspect ratio the ratio of the length of the electrolyte member to the length of the interconnector, should be maximised. This is because the longer the interconnector, the more expensive material is contained in the solid oxide fuel cell stack and the longer the support structure becomes the power density is reduced. Maximising the aspect ratio maximises the current density through the interconnectors. This makes the solid oxide fuel cell stack performance sensitive to electrode-interconnector contact resistance and to interconnector conductivity. An electrolyte member to interconnector aspect ratio of about 3 to 1 is used.

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Abstract

L'invention concerne un composant de pile à combustible à oxyde solide (12) comprenant une pluralité de piles à combustible à oxyde solide (24) disposées de façon espacée les unes par rapport aux autres, et en série électrique, sur une surface de la structure de support poreuse perméable au gaz (16). Chaque pile à combustible à oxyde solide (24) comprend un élément électrolytique dense étanche contre les gaz (28), une première électrode poreuse perméable au gaz (26) et une seconde électrode poreuse perméable au gaz (30). Chaque électrolyte (28) est en contact avec une des premières électrodes (26) correspondantes et chaque seconde électrode (30) est en contact avec un des électrolytes (28) correspondants. Chacune des premières électrodes (26) est en contact avec la surface de la structure de support (16). Les interconnecteurs (32), la couche d'étanchéité périphérique (34) et les électrolytes (28) sont conçus pour encapsuler toutes les premières électrodes (26) excepté les surfaces des premières électrodes (26) en contact avec la surface de la structure de support (16) pour empêcher toute fuite de réactif des premières électrodes (26).
PCT/GB2001/004410 2000-10-03 2001-10-02 Composant de pile a combustible a oxyde solide et son procede de fabrication WO2002029917A1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
JP2002533393A JP3934049B2 (ja) 2000-10-03 2001-10-02 固体酸化物形燃料電池構成部品及び固体酸化物形燃料電池構成部品の製造方法
AU2001292076A AU2001292076B2 (en) 2000-10-03 2001-10-02 A solid oxide fuel cell component and a method of manufacturing a solid oxide fuel cell component
ES01972299T ES2393978T3 (es) 2000-10-03 2001-10-02 Componente de pilas de combustible de óxido sólido y método de fabricación de un componente de pilas de combustible de óxido sólido
DK01972299.0T DK1332524T3 (da) 2000-10-03 2001-10-02 Fastoxidbrændselscellekomponent og fremgangsmåde til fremstilling af en fastoxidbrændselscellekomponent
EP01972299A EP1332524B1 (fr) 2000-10-03 2001-10-02 Composant de pile a combustible a oxyde solide et son procede de fabrication
AU9207601A AU9207601A (en) 2000-10-03 2001-10-02 A solid oxide fuel cell component and a method of manufacturing a solid oxide fuel cell component
CA2424681A CA2424681C (fr) 2000-10-03 2001-10-02 Composant de pile a combustible a oxyde solide et son procede de fabrication
US10/405,466 US7531260B2 (en) 2000-10-03 2003-11-25 Solid oxide fuel cell component and a method of manufacturing a solid oxide fuel cell component
US12/405,304 US7732075B2 (en) 2000-10-03 2009-03-17 Solid oxide fuel cell component and a method of manufacturing a solid oxide fuel cell component
US12/694,623 US7892691B2 (en) 2000-10-03 2010-01-27 Solid oxide fuel cell component and a method of manufacturing a solid oxide fuel cell component

Applications Claiming Priority (2)

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GBGB0024106.7A GB0024106D0 (en) 2000-10-03 2000-10-03 A solid oxide fuel cell stack and a method of manufacturing a solid oxide fuel cell stack
GB0024106.7 2000-10-03

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EP (1) EP1332524B1 (fr)
JP (1) JP3934049B2 (fr)
AU (2) AU2001292076B2 (fr)
CA (1) CA2424681C (fr)
DK (1) DK1332524T3 (fr)
ES (1) ES2393978T3 (fr)
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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007093759A1 (fr) 2006-02-14 2007-08-23 Rolls-Royce Plc Module de piles a combustible a oxyde solide dote d'une anode multicouche
US7482077B2 (en) 1999-11-16 2009-01-27 Northwestern University Direct hydrocarbon fuel cells
US7709124B2 (en) 2001-04-10 2010-05-04 Northwestern University Direct hydrocarbon fuel cells
US20100209802A1 (en) * 2006-04-03 2010-08-19 Bloom Energy Corporation Fuel cell stack components and materials
EP2424028A2 (fr) * 2009-04-20 2012-02-29 POSTECH Academy-Industry Foundation Bloc pour une pile à combustible à oxyde solide utilisant une structure tubulaire plate
US20120321984A1 (en) * 2011-06-15 2012-12-20 Richard Goettler Fuel cell system with interconnect
EP2562861A1 (fr) * 2007-11-08 2013-02-27 Alan Devoe Système de piles à combustible à oxyde solide sur support céramique
EP2795708A4 (fr) * 2011-12-22 2015-05-20 Saint Gobain Ceramics Interconnexions de pile à combustible à oxyde solide comprenant un matériau d'interconnexion céramique et du zircone partiellement stabilisé
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US7531260B2 (en) 2009-05-12
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CA2424681A1 (fr) 2002-04-11
EP1332524B1 (fr) 2012-08-29
US20090194219A1 (en) 2009-08-06
AU2001292076B2 (en) 2006-05-11
AU9207601A (en) 2002-04-15
ES2393978T3 (es) 2013-01-03
US7892691B2 (en) 2011-02-22
US7732075B2 (en) 2010-06-08
CA2424681C (fr) 2011-01-04
US20100129727A1 (en) 2010-05-27
DK1332524T3 (da) 2012-12-17
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JP3934049B2 (ja) 2007-06-20
US20040076867A1 (en) 2004-04-22

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